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Autor:
Gligorijević Nikola I., Rodić Vesna Ž., Živković Saša Ž., Pavković Bojan M., Nikolić Momčilo M., Kozomara Stevan M., Subotić Sredoje D.
Publikováno v:
Hemijska Industrija, Vol 70, Iss 5, Pp 581-594 (2016)
This paper presents the procedure of uniaxial mechanical characterization of composite solid rocket propellant based on hydroxy-terminated polybutadiene (HTPB), whose mechanical properties strongly depend on temperature, strain rate, natural aging
Externí odkaz:
https://doaj.org/article/e5d45f27b60142e4b51fa2fc474e9e5f